Laboratory study of rotationally inelastic collisions of CO2 at low temperatures.

C. Álvarez, G. Tejeda, J. M. Fernández
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Abstract

The rotational relaxation of CO2 by inelastic collisions has been studied in three supersonic jets. The jets were probed by means of Raman spectroscopy with high spectral and spatial resolutions, measuring the rotational populations and the total number density. The time evolution of the rotational populations was analyzed by means of a kinetic master equation, with the help of the energy-corrected sudden power law to relate the numerous state-to-state rate (STS rates) coefficients. In the thermal range investigated, 60-260 K, the STS rates decrease with increasing temperature and with increasing change in the rotational quantum number. Other quantities of interest for fluid dynamics, such as the rotational collision number, the relaxation cross section, and the bulk viscosity, have been derived from the STS rates.
低温下二氧化碳旋转非弹性碰撞的实验室研究。
在三个超音速喷流中研究了非弹性碰撞导致的二氧化碳旋转弛豫。通过高光谱和高空间分辨率的拉曼光谱对喷流进行了探测,测量了旋转群和总数量密度。通过动力学主方程分析了旋转群的时间演化,并借助能量校正突变幂律将众多状态-状态速率(STS速率)系数联系起来。在所研究的温度范围(60-260 K)内,STS 率随着温度的升高和旋转量子数的变化而降低。从 STS 速率还可以推导出流体动力学的其他相关量,如旋转碰撞数、弛豫截面和体积粘度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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